N954CB

Substantial
None

Brubaker F1S/N: 116

Accident Details

Date
Thursday, September 11, 2008
NTSB Number
LAX08CA293
Location
Truckee, CA
Event ID
20081003X17546
Coordinates
39.318611, -120.136947
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The failure of the bolts securing the tail wheel to its attach point that resulted in a loss of directional control.

Aircraft Information

Registration
Make
BRUBAKER
Serial Number
116
Engine Type
Reciprocating
Year Built
2005
Model / ICAO
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
BRUBAKER F1

Registered Owner (Current)

Name
AERO SERVICES LC
Address
2053 SOUTH 1640 WEST
City
WOODS CROSS
State / Zip Code
UT 84087-2334
Country
United States

Analysis

On September 10, 2008, about 1710 Pacific daylight time, an experimental amateur built Brubaker F1, N954CB, ground looped during landing at Truckee-Tahoe Airport (TRK), Truckee, California. The pilot/owner was operating the airplane under the provisions of 14 Code of Federal Regulations (CFR) Part 91. The certificated private pilot and one passenger were not injured; the airplane sustained substantial damage to the left wing tip. The cross-country personal flight departed Bountiful, Utah, about 1530. Visual meteorological conditions prevailed, and no flight plan had been filed.

The pilot reported that during a normal landing using runway 10 the airplane veered off to the right side of the runway when the tail wheel made runway contact. The pilot attempted to maintain directional control by applying full left rudder, but his rudder control inputs were ineffective.

The airplane sustained substantial damage to the left wing tip, the left landing gear, and the tail wheel.

The pilot stated that the airplane and engine had no mechanical failures or malfunctions during the flight.

The pilot submitted a Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2) on September 16, 2008. On October 3, 2008, the pilot submitted a modification to the original report following further examination of the airplane. The pilot reported that it appeared that the AN3 through bolts, which attach the tail wheel assembly to the tail spring, were sheared.

According to FAA Advisory Circular AC 20-27F, Certification and Operation of Amateur-Built Aircraft, "Amateur builders are free to develop their own designs or build from existing designs. We do not approve these designs and it would be impractical to develop design standards for the wide variety of design configurations, created by designers, kit manufacturers, and amateur builders."

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX08CA293